Impact Angle Control Guidance of Glide-Capable Munition Using a Vector Field Approach.
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| Title: | Impact Angle Control Guidance of Glide-Capable Munition Using a Vector Field Approach. |
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| Authors: | Lee, Suwon1 (AUTHOR) lsw7169@snu.ac.kr, Kim, Youdan2 (AUTHOR) ydkim@snu.ac.kr, Song, Chanho3 (AUTHOR) chanho.song@lignex1.com |
| Source: | IEEE Transactions on Aerospace & Electronic Systems. Apr2021, Vol. 57 Issue 2, p1069-1083. 15p. |
| Subjects: | Military weapons, Vector fields, Terminal velocity, Heuristic algorithms, Computer simulation |
| Abstract: | A vector field-based guidance law is proposed for the speed and impact angle control of an unpowered, glide-capable air-to-ground munition. An artificial 3-D space is designed for the glider vehicle to satisfy the terminal constraints. The glider vehicle is guided to the target position by the proposed vector field-based guidance law while satisfying the desired impact angle and final speed constraints. In the numerical simulations, various wind conditions are considered to demonstrate the performance of the proposed guidance law. [ABSTRACT FROM AUTHOR] |
| Copyright of IEEE Transactions on Aerospace & Electronic Systems is the property of IEEE and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) | |
| Database: | Engineering Source |
| FullText | Text: Availability: 0 |
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| Header | DbId: egs DbLabel: Engineering Source An: 149806595 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: Impact Angle Control Guidance of Glide-Capable Munition Using a Vector Field Approach. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Lee%2C+Suwon%22">Lee, Suwon</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> lsw7169@snu.ac.kr</i><br /><searchLink fieldCode="AR" term="%22Kim%2C+Youdan%22">Kim, Youdan</searchLink><relatesTo>2</relatesTo> (AUTHOR)<i> ydkim@snu.ac.kr</i><br /><searchLink fieldCode="AR" term="%22Song%2C+Chanho%22">Song, Chanho</searchLink><relatesTo>3</relatesTo> (AUTHOR)<i> chanho.song@lignex1.com</i> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22IEEE+Transactions+on+Aerospace+%26+Electronic+Systems%22">IEEE Transactions on Aerospace & Electronic Systems</searchLink>. Apr2021, Vol. 57 Issue 2, p1069-1083. 15p. – Name: Subject Label: Subjects Group: Su Data: <searchLink fieldCode="DE" term="%22Military+weapons%22">Military weapons</searchLink><br /><searchLink fieldCode="DE" term="%22Vector+fields%22">Vector fields</searchLink><br /><searchLink fieldCode="DE" term="%22Terminal+velocity%22">Terminal velocity</searchLink><br /><searchLink fieldCode="DE" term="%22Heuristic+algorithms%22">Heuristic algorithms</searchLink><br /><searchLink fieldCode="DE" term="%22Computer+simulation%22">Computer simulation</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: A vector field-based guidance law is proposed for the speed and impact angle control of an unpowered, glide-capable air-to-ground munition. An artificial 3-D space is designed for the glider vehicle to satisfy the terminal constraints. The glider vehicle is guided to the target position by the proposed vector field-based guidance law while satisfying the desired impact angle and final speed constraints. In the numerical simulations, various wind conditions are considered to demonstrate the performance of the proposed guidance law. [ABSTRACT FROM AUTHOR] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of IEEE Transactions on Aerospace & Electronic Systems is the property of IEEE and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.) |
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| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.1109/TAES.2020.3037399 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 15 StartPage: 1069 Subjects: – SubjectFull: Military weapons Type: general – SubjectFull: Vector fields Type: general – SubjectFull: Terminal velocity Type: general – SubjectFull: Heuristic algorithms Type: general – SubjectFull: Computer simulation Type: general Titles: – TitleFull: Impact Angle Control Guidance of Glide-Capable Munition Using a Vector Field Approach. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Lee, Suwon – PersonEntity: Name: NameFull: Kim, Youdan – PersonEntity: Name: NameFull: Song, Chanho IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 04 Text: Apr2021 Type: published Y: 2021 Identifiers: – Type: issn-print Value: 00189251 Numbering: – Type: volume Value: 57 – Type: issue Value: 2 Titles: – TitleFull: IEEE Transactions on Aerospace & Electronic Systems Type: main |
| ResultId | 1 |
